AD/ROBIN/4 - Aileron/Flap Support Brackets - Inspection and Reinforcement
© 2026 Zoe. All rights reserved.
Zoe is a legal information platform. Always consult the Federal Register of Legislation for authoritative text.
AD/ROBIN/4 - Aileron/Flap Support Brackets - Inspection and Reinforcement
Start here
Turn the raw legal text into a practical explanation grounded in AD/ROBIN/4 - Aileron/Flap Support Brackets - Inspection and Reinforcement.
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Robin Aviation Series Aeroplanes
AD/ROBIN/4 Aileron/Flap Support Brackets - Inspection
and Reinforcement
10/82
Applicability: All model R2000.
Document: Avions Pierre Robin SB No. 90.
Compliance: Within 100 hours time in service after 31 October, 1982.
Background: The Manufacturer has reported cracking adjacent to the attachment points of the left and right aileron/flap common support brackets and corresponding wing skin areas.